Geometry-Independent Hypersonic BoundaryLayer Transition Prediction

One of the fundamental challenges of fielding and maneuvering a hypersonic vehicle is predicting the large changes in heat transfer and aerodynamic performance associated with the transition of the surface boundary-layer flow from laminar to turbulent during flight. Legacy methods for analyzing boun...

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Veröffentlicht in:	Johns Hopkins APL technical digest 2022-01, Vol.36 (2), p.202
Hauptverfasser:	Araya, Daniel B, Bitter, Neal P, Alkandry, Hicham
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary layer flow Boundary layer transition Flow distribution Geometric constraints Hypersonic flow Hypersonic vehicles Input output analysis Laminar flow R&D Research & development Software
Online-Zugang:	Volltext
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